公开(公告)号：US06226974B1

公开(公告)日：2001-05-08

申请号：US09339956

申请日：1999-06-25

申请人： Philip Lynn Andrew ,  Paul Thomas Marks ,  Daniel Robert Dwyer ,  John David Stampfli ,  Joseph Anthony Cotroneo ,  Harold Edward Miller ,  Ronald Richard Wesorick

发明人： Philip Lynn Andrew ,  Paul Thomas Marks ,  Daniel Robert Dwyer ,  John David Stampfli ,  Joseph Anthony Cotroneo ,  Harold Edward Miller ,  Ronald Richard Wesorick

IPC分类号： F02C1310

CPC分类号： F02C9/28 ,  F04D27/02 ,  F05D2270/05 ,  Y02E20/16

摘要： A gas turbine operational strategy is provided for the optimization of ISO-Day rated performance. The invention is realized by setting the nominal operating line equal to or slightly below the operating limit line, so that ISO full load performance is maximized. Thus, the first stage turbine nozzle throat area is sized such that, without inlet bleed heat addition, and at Base-Load pressure ratio and firing temperature, the compressor operates within its operational limits on a ISO day. As ambient conditions change, levels of inlet bleed heat and firing temperature are controlled and the inlet guide vane angle is set whereby the nominal operating line is equal to or slightly below the operating limit line.

摘要翻译： 提供燃气轮机操作策略，以优化ISO-Day的性能。 本发明通过将标称操作线设置为等于或稍低于操作限制线来实现，使得ISO满载性能最大化。 因此，第一级涡轮喷嘴喉部区域的尺寸使得在没有入口放热加入的情况下，并且在基本负载压力比和烧制温度下，压缩机在ISO日的运行限度内运行。 随着环境条件的变化，入口排放热量和燃烧温度的水平被控制，并且入口导向叶片角度被设定，由此标称操作线等于或略低于操作极限线。

公开(公告)号：US06464461B2

公开(公告)日：2002-10-15

申请号：US09731982

申请日：2000-12-08

申请人： Ian David Wilson ,  Kevin Joseph Barb ,  Ming Cheng Li ,  Susan Marie Hyde ,  Thomas Charles Mashey ,  Ronald Richard Wesorick ,  Christopher Charles Glynn ,  Martin C. Hemsworth

发明人： Ian David Wilson ,  Kevin Joseph Barb ,  Ming Cheng Li ,  Susan Marie Hyde ,  Thomas Charles Mashey ,  Ronald Richard Wesorick ,  Christopher Charles Glynn ,  Martin C. Hemsworth

IPC分类号： F01D508

CPC分类号： F01D5/085 ,  F02C7/16 ,  F05D2260/2322 ,  Y02T50/676

摘要： The steam cooling circuit for a gas turbine includes a bore tube assembly supplying steam to circumferentially spaced radial tubes coupled to supply elbows for transitioning the radial steam flow in an axial direction along steam supply tubes adjacent the rim of the rotor. The supply tubes supply steam to circumferentially spaced manifold segments located on the aft side of the 1-2 spacer for supplying steam to the buckets of the first and second stages. Spent return steam from these buckets flows to a plurality of circumferentially spaced return manifold segments disposed on the forward face of the 1-2 spacer. Crossover tubes couple the steam supply from the steam supply manifold segments through the 1-2 spacer to the buckets of the first stage. Crossover tubes through the 1-2 spacer also return steam from the buckets of the second stage to the return manifold segments. Axially extending return tubes convey spent cooling steam from the return manifold segments to radial tubes via return elbows.

摘要翻译： 用于燃气涡轮机的蒸汽冷却回路包括孔管组件，其将周向间隔开的径向管供给蒸汽，所述径向管连接到供应弯头，以沿着与沿转子边缘的蒸汽供应管沿轴向方向转换径向蒸汽流。 供应管将位于1-2间隔物的后侧的周向隔开的歧管段供应蒸汽，以将蒸汽供应到第一和第二级的桶。 来自这些铲斗的废水返回蒸汽流向设置在1-2间隔物的前表面上的多个周向间隔开的返回歧管段。 交叉管将来自蒸汽供应歧管段的蒸汽供应通过1-2间隔件连接到第一级的桶。 通过1-2间隔物的交叉管还将蒸汽从第二级的桶返回到回流歧管段。 轴向延伸的回流管通过返回弯头将废冷却蒸汽从返回歧管段传送到径向管。